STARLINK-1090, 44968
Orbit data source: Space-Track
STARLINK-1090, 44968 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 07 Jan 2020 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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44968 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 STARLINK-1090
1 44968U 20001BG 25287.59799978 .00000858 00000-0 76494-4 0 9996
2 44968 53.0531 242.4509 0001394 87.5168 272.5980 15.06395071318392
TLE epoch observation values (Epoch: 2025-10-14T14:21:07.180Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #1 in the year 2020 (2020-01-07 UTC)
STARLINK-1090 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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4 mins | 2025-10-15 22:21:16.636Z | 161.215° S | 2025-10-15 22:23:16.636Z | 126.8° SE | 17.382° | 2025-10-15 22:25:16.636Z | 92.718° ESE |
6 mins | 2025-10-16 00:00:16.636Z | 250.039° W | 2025-10-16 00:02:16.636Z | 312.072° NW | 41.252° | 2025-10-16 00:06:16.636Z | 44.33° NE |
4 mins | 2025-10-16 01:41:16.636Z | 318.84° NNW | 2025-10-16 01:42:16.636Z | 336.602° NNW | 16.838° | 2025-10-16 01:45:16.636Z | 24.913° NE |
5 mins | 2025-10-16 05:02:16.636Z | 345.665° N | 2025-10-16 05:04:16.636Z | 28.907° NE | 23.424° | 2025-10-16 05:07:16.636Z | 80.579° E |
6 mins | 2025-10-16 06:41:16.636Z | 299.162° NW | 2025-10-16 06:44:16.636Z | 195.725° SSW | 40.441° | 2025-10-16 06:47:16.636Z | 145.134° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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